▸Orbital parameters

Orbit class	LEO
Inclination	88.9723°
Eccentricity	0.0010982
Period	106.6 min
Apogee	1,077 km
Perigee	1,060 km
Mean motion	13.51016740 rev/day
RAAN	298.5039°
Arg of perigee	245.3950°
Mean anomaly	114.6057°
B*	2.1958e-4
Rev at epoch	7,534

▸Two-line element set (TLE)

EPOCH Jul 7, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 63168U 25046K 26188.15942208 .00000154 00000-0 21958-3 0 9995

2 63168 88.9723 298.5039 0010982 245.3950 114.6057 13.51016740 75348

▸ source OMM (JSON)

{
  "OBJECT_NAME": "QIANFAN-82",
  "OBJECT_ID": "2025-046K",
  "EPOCH": "2026-07-07T03:49:34.068+00:00",
  "MEAN_MOTION": 13.5101674,
  "ECCENTRICITY": 0.0010982,
  "INCLINATION": 88.9723,
  "RA_OF_ASC_NODE": 298.5039,
  "ARG_OF_PERICENTER": 245.395,
  "MEAN_ANOMALY": 114.6057,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 63168,
  "REV_AT_EPOCH": 7534,
  "BSTAR": 0.00021958,
  "MEAN_MOTION_DOT": 0.00000154,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	QIANFAN-82
Operator	Shanghai Spacecom Satellite Technology LtdHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Mar 11, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	267HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/63168

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.